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Rotating Detonation Engine Performance Model for Rocket Applications
Author(s) -
David P. Stechmann,
Stephen D. Heister,
Alexis Harroun
Publication year - 2018
Publication title -
journal of spacecraft and rockets
Language(s) - Uncategorized
Resource type - Journals
SCImago Journal Rank - 0.758
H-Index - 79
eISSN - 1533-6794
pISSN - 0022-4650
DOI - 10.2514/1.a34313
Subject(s) - rocket engine , specific impulse , nozzle , detonation , thrust , aerospace engineering , combustion chamber , rocket engine nozzle , propellant , ramjet , booster (rocketry) , nuclear engineering , body orifice , mechanical engineering , mechanics , automotive engineering , combustion , engineering , physics , explosive material , chemistry , combustor , organic chemistry

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